Weapon location by acoustic-optic sensor fusion

ABSTRACT

An weapon localization system for determining the location of hostile weapon fire. In one embodiment, the weapon localization system includes acoustical detection means for detecting energy of a first frequency originating from said hostile weapon fire; and for transmitting a first set of data describing the location of said hostile weapon fire; optical detection means for detecting energy of a second frequency originating from said hostile weapon fire, and for transmitting a second set of data describing the location of said hostile weapon fire; and processing means coupled to said acoustical and said optical detection means for receiving said first and said second set of data and for determining whether said location of said first set of data match said location of second set of data and for generating a signal output if said match occurs.

This application is a CIP of 09/292,082, filed Apr. 14, 1999 now U.S.Pat. No. 6,215,731 which is a CIP of 08/834,754, filed Apr. 30, 1997 nowU.S. Pat. No. 5,970,024.

1. FIELD OF THE INVENTION

The present invention relates to a system and method which combinesvarious detection, location and tracking technologies in order tolocalize, calculate, determine, and/or track the source of hostileweapons fire such as that emanating from a sniper or an overhead“top-attack” weapon and to employ countermeasures adapted to protect avehicle and/or personnel from this hostile weapons fire.

2. Background of the Invention

Previous weapon location systems (as used throughout this Application,the term “system” refers to a combination, in one embodiment, ofhardware, software, and/or firmware which cooperates to perform one ormore applications or functions) used either a purely or substantiallysingular acoustical detection apparatus or techniques or a purely orsubstantially singular optical detection apparatuses and/or techniquesto locate the source of hostile weapon fire. Due to the problems and/ordrawbacks associated with purely acoustical and purely optical detectiontechniques or substantially pure or singular technology techniques, thepresent invention combines the two concepts or technologies in order toutilize the advantages and substantially eliminate the disadvantages ofeach technology. Applicant has found that the combination of acousticaland optical as well as other detection and tracking mechanisms greatlyenhances the overall detection capability of the system. Applicantbelieves that there was, prior to Applicant's, invention, no and/orsubstantially little or substantially no motivation to combine thesetechniques in the manner done by Applicant and which adequately achievedthe results and/or goal of Applicant's invention.

Acoustical detection systems generally determine the direction and/orlocation of hostile weapon fire by measuring and/or calculating thevarious times of arrival of “sound” or acoustical energy generated bythe hostile fire by the use of generally and equally spaced microphonesformed or placed in a microphone array. Most prior acoustical hostileweapons fire detection and/or location systems are characterized bygenerally omnidirectional detection, only moderate accuracy and asubstantially minimal false alarm rate. While such prior acousticalsystems provide useful information for many applications, purely and/orsubstantially pure acoustical detection systems are not entirelyappropriate for certain applications, such as applications involving thedetection of the firing of supersonic and/or substantially supersonicprojectiles, and the tracking of overhead “top attack” weapons. That is,supersonic projectiles arrive at the target prior to the arrival of theacoustical energy generated by the firing of these supersonicprojectiles. Thus, an immediate counter-measure launch, necessary todestroy the incoming supersonic missiles, is generally not possible whena purely or singular acoustical system is used to detect the presenceand/or location of such supersonic enemy fire. Additionally, it is wellknown that acoustical detection systems: can have a relatively largeerror in the determination of the location of the hostile weapon. In thepast, this was not really a problem since offensive countermeasureswhich were used to destroy the hostile weapon usually comprised one ormore missiles which destroyed a relatively large area. This wide area ofdestruction mostly and adequately compensated for the errant locationdata provided by the acoustical detection and/or location systems.However, war has changed. Oftentimes snipers, located within relativelydensely populated areas are now encountered. Hence, large destructivecountermeasures, necessary to compensate for errant locationcalculations, are generally not appropriate since they might hurt orkill many innocent people and destroy many valuable and historicbuildings and/or other structures.

Optical detection systems generally determine the location and/ordirection of hostile weapons fire by observing and/or sensing theposition of the optical energy released or generated when a weapon isdischarged. Most optical systems are characterized by relatively highaccuracy, relatively high amounts or levels of false alarms and a ratherlimited field of view. Purely optical systems are also of rather limitedvalue in some ambient light conditions where distinguishing the flash ofa weapon from false flashes or other types of visible radiation isdifficult. Purely optical systems are also of rather limited value wherea weapon is obstructed or outside of the optical system's field of view.Hence, these prior optical detection systems were used only in very fewspecific applications, mainly due to their relatively high false alarmrate. Heretobefore, only one type of these systems was used todetermine/calculate the location of adverse weaponry. No one, prior, toApplicant's discovery and/or invention, had realized the benefit ofcombining these two types of dissimilar systems in a manner which wouldovercome the drawbacks of each of these systems and provide a morerobust system.

That is, Applicant was the first to realize that great accuracy andusefulness could be achieved by first using an acoustical system todetermine the general location of the hostile weapons fire, a functionthat such prior acoustical systems performed relatively well, and thenusing an optical system or referring to or reviewing captured opticaldata in order to further refine the location within the fieldestablished by the acoustical system. In this manner, the relativelynotorious “false alarms” associated with the optical systems could beminimized since only the optical data which emanates and/or is generatedfrom the field of view formed or “fixed” by the acoustical techniquewould be reviewed. Moreover, the concomitant use of optical system datacould allow even supersonic projectiles to be detected. This newcombined system thus allows great accuracy which is necessary whendetecting hostile weapons fire in cities and other areas in whichgreatly destructive missile counteroffensive apparatuses cannot be used.

Importantly, Applicant has discovered that the present invention isespecially useful in detecting, tracking and countering attacks fromoverhead or “top attack” weapons. It is known that armored militaryvehicles generally have their strongest armor (greatest thickness) ontheir respective sides, and on their respective front and back surfaces.The armor covering the top and the bottom of armored vehicles isgenerally somewhat thinner, less protective, and generally moresusceptible to penetration than the armor on the sides of such vehicles.As a result, armored vehicles are generally known and/or thought to bemore difficult to attack using weapons that have horizontaltrajectories, and are more vulnerable to weapons following and/orexhibiting steep travel trajectories and weapons which may be launchedor fired from directly above these vehicles. Until relatively recently,the “threat” weapons or the weapons used to attack armored vehicles havebeen almost exclusively horizontal trajectory weapons.

However, to exploit the higher vulnerability of the “topside” armor ofmilitary armored mobile vehicles, new weapons have been developed.Generally, these weapons can direct shaped charges and launchprojectiles towards armored vehicles from a location directly above thevehicle.

A diagram of the travelling and/or firing trajectory or path 102 of onesuch weapon and the significant events of its arming sequence is shownin FIG. 12. As illustrated in FIG. 12, the overhead weapon 120 comprisesa delivery device 100, typically a 155 mm artillery projectile, which isinitially launched and carries or “delivers” the overhead or “topattack” weapon portion 104 to a point approximately 1200 meters or moreabove the target vehicle 118. At this point, top attack weapon portion104 generally comprising a “package” containing two submunition“packages” 106, 108 is expelled from the delivery projectile 100 by asmall explosive charge (i.e., “the main event”). This is followed almostimmediately by a first “band cutter” event where a small explosive (notshown) cuts a steel band 109 usually connecting packages 106, 108,effective to separate the two submunition packages 106, 108. Eachpackage relatively immediately deploys a parachute-like fabricdecelerator 110 (e.g., a “Rapid Air Inflatable Decelerator” (“RAID”)),to slow the horizontal speed of each submunition 106, 108 from thehorizontal launch speed of approximately mach 1 to essentially zero.This causes each submunition 106, 108 to fall along a verticaltrajectory. After each of the two submunitions 106, 108 has slowed to avertical trajectory, a small explosive charge in each submunition (notshown) performs a second band cutter task that is effective to cause thedeployment of a second parachute-like device 112 (e.g., a Vortex RingParachute (“VRP”)), from each submunition package. The VRP provides theplatform for vehicle target acquisition and attack by the submunition.At this point, each submunition will scan for a target (i.e., an armoredvehicle 118) in a predetermined area below the submunition using heatsensing, image recognition or another suitable technology. Upon locatinga viable target, each submunition 106, 108 will fire a projectile orexplosive device (not shown) upon the target. The entire top attacksequence from “the main event” to the firing by submunitions 106, 108may take as long as 30 to 45 seconds.

Each of the afore-described events (i.e., the main event, the first bandcutter event, and the second band cutter event) generates an acousticalevent. The main event will also typically generate an optical flash thatis visible in the mid-wave IR band. Various falling objects have alsobeen observed with a mid-wave IR camera. The sensor fusion system of thepresent invention generally allows for generally reliable detection,tracking and countermeasure accuracy and results of such top-attackweapons which emit various acoustical and optical signals.

There is therefore a need for, and it is a principal object of thisinvention to provide, a weapon and/or hostile weapons firing locationand localization system which overcomes the aforementioned drawbacks ofthe prior substantially purely acoustical and substantially purelyoptical detection systems and which, in fact, combines the advantagesand the techniques of the two systems to achieve a system characterizedby general omnidirectional detection, a relatively low false alarm rate,relatively high accuracy and relatively immediate counter-measurecapability. In essence, Applicant has discovered that, one may utilizethe accuracy of infrared systems in combination with “gross” typelocation data specified by the acoustical systems to provide a verydesirable “fused” system. Applicant has further discovered that such acombination of systems can be further improved by using various trackingtechnologies which will allow a target to detect an overhead attack,take defensive action and direct a countermeasure. As used in thisApplication, the terms “location” and “localization” each mean thelocation of an entity (e.g. hostile weapons fire) as well as theprocesses to locate the firing entity. Thus, these words may be usedinterchangeably.

SUMMARY OF THE INVENTION

According to a first aspect of the present invention, a weapon locationand/or detection system is provided which combines an acousticaldetection system and an optical detection system to utilize theadvantages and substantially reduce and/or eliminate the disadvantagesof each technology.

According to a second aspect of the present invention, a weapon locationand/or detection system is provided which is designed to determine thelocation of hostile weapon fire and which generally has omnidirectionaldetection capability, a relatively low false alarm rate, relatively highaccuracy and relatively immediate counter-measure capability.

According to a third aspect of the present invention, a weapon location,detection and tracking system is provided which is designed to detect anoverhead attack, take defensive action and direct a countermeasure.

In one embodiment of the present invention, a weapon location and/ordetection system adapted to determine the location of hostile weaponfire is provided. The system comprises acoustical detection means fordetecting energy of a first frequency originating from the firing of thehostile weapon, and for creating and transmitting a first set of datadescribing the location of the hostile weapon; optical detection meansfor detecting energy of a second frequency originating from the firingof the hostile weapon, and for creating and transmitting a second set ofdata describing the location of the hostile weapon; and processing meanscommunicatively coupled to the acoustical and the optical detectionmeans, for receiving the first and the second set of data and forcomparing the first and second sets of data and for generating a signaloutput if the comparison yields and/or results in a match.

In another embodiment of the present invention a weapon location systemadapted to determine the location of hostile weapon fire is provided. Inthis alternate embodiment the system comprises acoustical detectionmeans for detecting energy of a first frequency originating from hostileweapon fire and for transmitting a first set of data describing thelocation of said hostile weapon fire; laser detection meanscommunicatively coupled to the acoustical detection means for receivingthe first set of data, for scanning the location described by the firstset of data, for detecting particles associated with discharge of saidhostile weapon fire, and for transmitting a second set of datadescribing the location of said particles; and processing meanscommunicatively coupled to the acoustical and the optical detectionmeans, for receiving said first and said second set of data, and fordetermining whether the location of the first set of data match orcorrespond to the location of the second set of data and for generatinga signal output if a match and/or correspondence occurs.

According to yet another embodiment of the invention a methodology fordetermining the location of hostile weapons fire is provided. In a firstaspect of this methodology embodiment, the method comprises the steps ofsensing acoustical energy associated and/or generated from the hostileweapons fire; sensing optical energy associated and/or generated fromthe hostile weapons fire; calculating a first location using only thesensed acoustical energy; calculating a second location using only thesensed optical energy; comparing the first and second locations; andproviding an output signal if the first location is substantiallysimilar to the second location.

Further objects, features, and advantages of the present invention willbecome apparent from any consideration of the following description andthe appended claims, when taken in conjunction with the accompanyingdrawings.

BRIEF DESCRIPTION OF THE DRAWINGS

For a fuller and more complete understanding of the nature and objectsof the present invention, reference should be had to the followingdrawings in which:

FIG. 1 is a block diagram of the preferred embodiment of the presentinvention;

FIG. 2 is a block diagram of the operation of the processing means usedin the preferred embodiment of the present invention;

FIG. 3 is a block diagram of an acoustical detection means used in thepreferred embodiment of the present invention;

FIG. 4 is a top view of a microphone array which may be used in thepresent invention;

FIG. 5 is a block diagram of an optical detection means used in thepreferred embodiment of the invention;

FIG. 6 is a perspective view of components of the preferred embodimentof the present invention employed on the exterior of a vehicle;

FIG. 7 is a side view of components of the preferred embodiment of thepresent invention employed within a vehicle;

FIG. 8 is a top view of a camera array which may be used in the presentinvention;

FIG. 9 is a block diagram of the operation of a second embodiment of thepresent invention;

FIG. 10 is block diagram of a laser detection system used in the secondembodiment of the present invention;

FIG. 11 is a block diagram of the operation of the processing means usedin the a second embodiment of the present invention;

FIG. 12 illustrates the trajectory of a typical top attack weapon andthe main, and first and second band cutting events;

FIG. 13 is a block diagram of a preferred embodiment of a top attack,detection and tracking system;

FIG. 14 is a block diagram of a second embodiment of a top attackdetection and tracking system; and

FIG. 15 is a block diagram of a third embodiment of a top attackdetection and tracking system.

FIG. 16 is a block diagram of a fourth embodiment of a top attackdetection and tracking system.

FIG. 17 is a diagram of a top attack detection and tracking system.

DETAILED DESCRIPTION OF THE INVENTION

Referring now to FIG. 1, there is shown a block diagram of a weaponand/or hostile fire location and/or detection system 2 which is made inaccordance with the preferred embodiment of this invention. As shown,weapon location/detection system 2 includes an acoustical detectionmeans 4, an optical detection means 6, a processing means 8, and anoutput providing means 10.

According to one aspect of the system 2, acoustical detection means 4comprises, for example and without limitation, those acoustical systems,devices, and/or apparatuses which are more fully described in U.S. Pat.No. 5,258,962 entitled “Acoustic Projectile Trajectory EvaluationDevice”, invented by Lasse Karlsen; U.S. Pat. No. 4,350,881, entitled“Projectile Position Detection Apparatus”, and invented by Knight etal.; and U.S. Pat. No. 4,885,725, entitled “Position Measuring Apparatusand Method”, and invented by McCarthy et al. Each of these United StatesPatents is hereby fully and completely incorporated by reference as iffully and completely set forth herein, word for word and paragraph byparagraph.

FIG. 3 illustrates one exemplary type of acoustical detection system 24which may be used in and by the invention. As shown, acousticaldetection system 24 comprises and/or includes a microphone array 26(pictured alone in FIG. 4) and an acoustical processor 28. Each of themicrophones arranged within microphone array 26 operates and is adaptedto receive incoming acoustical energy 25 of a first acoustical or“sound” frequency (most probably in the range of about 300 hz to about15,000 hz) originating and/or associated with the firing of a hostileweapon, and to transmit a separate signal 27 from each microphone 29 inmicrophone array 26 to an acoustical processor 28. Acoustical processor28, in the preferred embodiment of the invention comprises, amicroprocessor operating under stored program control and associatedoperating hardware and software. Such microprocessor assemblyarrangements are described more fully in the textbook entitled “ComputerArchitecture and Organization” which was authored by John P. Hayes,published by the. McGraw-Hill book company and having a libraryreference identification of I5BN 0-67-027363-4 and which is fully andcompletely incorporated herein by reference, word for word, andparagraph for paragraph. Specifically processor assembly 28 determinesand/or calculates the location of the source of the acoustical energy(e.g. the location of the weapon whose firing generated the energy) andcreates and transmits location data describing the hostile weaponrylocation to processing means 8 by use, in one embodiment, of algorithmsand other known mathematical operations described more fully in thepreviously incorporated United States Patents and which are known tothose skilled in this art.

Acoustical detection system 24, and more particularly processor orprocessor means 28, in the preferred embodiment of the invention,determines values such as time of energy arrival, azimuth,elevation/depression angle, and trajectory of the incoming acousticalenergy. The acoustical detection system 24 may also employ a filter (notshown) to distinguish and/or “block out” some of the various acousticalenergies received by microphone array 26 in order not to have processor28 errantly process non-weapons firing noises. That is, for example andin one embodiment, the filter will allow only those frequenciesassociated with a specific type of hostile weapons fire to reach thearray 26. Similarly, acoustical energy characteristics will vary witheach type of employed hostile weapon. Hence, filter designcharacteristics in acoustical detection system 24 will be varied tooptimize detection. Particularly, the filters will be designed/selectedin order to allow only the energies of the known hostile weapons systemsto be coupled to processor 28. The precise operation and calculations ofacoustical detection system 24 is more fully described and illustratedby the inventor in the aforementioned fully incorporated patentreferences. It is important to note that the invention is not limited touse with the exact acoustical detection systems described, in thesepreviously incorporated references. Applicant realizes that a number ofother acoustical detection systems can and should be used that wouldproduce substantially similar or even superior results and would notdepart from the spirit and scope of the invention and the inclusionand/or use of these previously described/incorporated acoustical systemembodiments in Applicant's invention should not be construed so as tolimit the nature of the described invention or in any manner affect thescope of the subjoined claims. For example and without limitation, theacoustical detection system 24 for this invention could use a threemicrophone array, a tetrahedral array, or another array forming a threedimensional solid. Such designs will provide direction similarly precisedetection and estimation and would require only appropriate revisions tothe signal processing algorithms employed by acoustical detection system24.

Optical detection means 6 used in the preferred embodiment of thisinvention may comprise a conventional and commercially available opticaldetection system, examples of which are more fully described in U.S.Pat. No. 3,944,167 entitled “Radiation Detection Apparatus” and inventedby Figler et al.; and U.S. Pat. No. 3,848,129 entitled “SpectralDiscriminating Radiation Detection Apparatus” and invented by, Figler etal. Each of these United States Patent references are fully andcompletely incorporated herein by reference as if fully and completelyset forth herein, word for word and paragraph by paragraph. One exampleof a suitable optical detection system is the commercially availablemodel IRC-160ST Staring-Mid Wavelength Infrared Camera, manufactured andsold by Cincinnati Electronics (Cincinnati, Ohio).

As shown in FIG. 5, the optical detection system 32 used in thepreferred embodiment of the present invention (corresponding in oneembodiment to optical detection means 6) comprises an infrared camera 34and an optical processor assembly 36 which, in one embodiment of theinvention, comprises a microprocessor assembly operating under storedprogram control. Such an assembly may be substantially similar to thepreviously described assembly 28 and described in the previouslyincorporated Hayes textbook reference.

Infrared camera 34 operates and/or functions to receive incoming energyof a second or “infrared” or visual type of frequency originating fromand/or associated with hostile weapon fire and upon receiving and/orsensing this incoming energy transmits a signal to an optical processor36. Optical processor 36 determines the location of the source of thehostile weapon fire and creates and/or transmits data describing thecalculated/determined location to processing means 8. Such calculationsand/or determination are made by use of, in one embodiment, algorithmsand mathematical analyses which are more fully described in the UnitedStates Patent references which are fully incorporated herein byreference and which are known to those skilled in this art.

Weapon location/detection system 2 may also function and/or operate witha camera assembly 501 (pictured alone in FIG. 17) replacing singularand/or substantially singular infrared camera 34. Camera assembly 501comprises optical reflector surface 504 and camera 505. Reflectorsurface 504 is specular and in the preferred embodiment has the shape ofa figure of revolution about its vertical axis of revolution 508 therebyallowing it to receive optical energy from any azimuth and reflect thisoptical energy downwards to camera 506. Camera 505 operates and/orfunctions to receive incoming optical energy that is generated byhostile weapon fire of an “infrared” and/or visual type of frequency andis reflected from reflector surface 504. Other shapes for reflectorsurface 509 are possible within the spirit of this invention.

Optical energy source 503 emits optical energy 502 that strikesreflector surface 504 at principal reflection point 509 where opticalenergy 502 is diverted to camera 505 that senses reflected opticalenergy 506 received from principal reflection point 509 on reflectorsurface 504. Camera 505 upon receiving and/or sensing this incomingoptical energy transmits a signal to optical processor 36 thatdetermines the location of principal reflection point 509 and thencalculates direction from reflection point 509 to optical energy source503 by using a microprocessor which may substantially correspond to thepreviously described microprocessor assembly 36 acting under storedprogram control that follows an established mathematical relationshipunderstood by one with ordinary skills in the art.

In such a case repositioning means. 22 is not included in weaponlocalization system 2, nor is it required, since camera assembly 501covers all possible fields of view. Other then the absence ofrepositioning means 22 weapon localization system 2 with camera array501 operates in substantially the same manner as previously described.

Particularly, as more fully described in these prior incorporatedreferences, optical detection system 32 will determine values such asazimuth, time of occurrence and elevation/depression angle of theincoming energy. The precise operation and calculations of opticaldetection system 32, are more fully described in the aforementionedfully incorporated references. The invention is not limited to use withthe aforementioned optical detection system. Certain design details willvary depending upon the class of hostile weapons to be detected andlocalized. For example, and without limitation, certain weapons such asantitank missiles may have a stronger signature in one of the infrared,visible or ultraviolet bands. The camera employed in weapon localizationsystem 2 will correspond to the frequency of the desired weapon.Furthermore, Applicant realizes, as should one of ordinary skill in theart, that a number of other optical detection systems can be used thatwould produce substantially similar results and not depart from thespirit of the invention.

To understand the operation of weapon localization system 2, referenceis now made to FIG. 2 which illustrates the operation of the processingmeans 8 used in the preferred embodiment of the invention. It should beobvious to those skilled in the art that other types of operations arepossible. In the preferred embodiment of the invention, processing means8 is a microprocessor assembly acting under stored program control andwhich may substantially correspond to the previously describedmicroprocessor assemblies 24 and 28. One example of an acceptableprocessor for use in these assemblies is a commercially availablePentium® type processor manufactured by Intel Corporation.

According to one aspect of the present invention, processing means 8 iscommunicatively and physically coupled to processing means 28 and 36 andreceives first and second sets of data from acoustical detection system24 and optical detection system 32, respectively. Processing means 8records the location and time of occurrence of each set of data receivedand outputs the data to a display, as indicated by software operationblocks 12, 14. Processing means 8 holds and/or stores all locations fromthe second set of data for a predetermined period of time and comparesthese stored locations with locations from the first set of data, asindicated by block 16. A “match” or “hit” is indicated when a locationand time from the first set of data (hereinafter referred to as the“acoustical event”) fall within a predetermined range of a location andtime from the second set of data (hereinafter referred to as the “opticevent”). If a match is detected, processing means 8 will generate asignal output, as indicated by block 16. Indicating that both theacoustical and infrared systems “match” and correspond to a hostileweapons location. In the preferred embodiment of the invention, thesignal output will be transmitted to a display, indicated by block 14,where it will be shown in a manner different from the displayedlocations of unmatched data points. The signal output will also indicatewhether the acoustical event occurred before the optically sensed event.When the acoustical event occurs before the optically sensed event, theoptical event actually represents a subsequent attack from the samelocation, since optical energy generally reaches the observer beforeacoustical energy and the associated missile. In such a case, acounter-measure against the incoming missile may be launched. In thepreferred embodiment of the invention, a counter-measure device,indicated by block 18, receives the signal output and is designed toposition a weapon and fire a counter-attack at the predicted location ofthe missile and/or the missile's origin. Data such as azimuth,elevation/depression angle, arrival angle and trajectory of the incomingenergy can be used to calculate the path of the missile and intercept itbefore arrival.

If no matches are detected within a predetermined period of time, theunmatching locational data from the optical event will be discarded, asindicated by block 20, and the unmatching data from the acoustical eventwill be transmitted to a repositioning means, as indicated by block 20,22. As best shown in FIGS. 5 and 6, repositioning means 22 will rotateinfrared camera 34 so the field of view 40 of infrared camera 34 iscentered in the location of the acoustical event, thus ensuring a matchin the event of subsequent fire from that location. In this manner, theinfrared camera 34 is “keyed” to a specific area thereby reducing thefalse alarms and taking advantage of the relatively great accuracy ofthe optical detection means. In essence, the broad acoustical detectiontechniques and system is used to fix a rather coarse location and theoptical detection system is used to further refine this detection.

To passively determine the range or distance to the hostile weaponsfire, the invention uses a “flash-bang” analysis. In one embodiment,processing means 8 takes the second or optical data and notes the timeof its arrival. Then, processing means 8 takes the first or acousticaldata which arrives later than the optical data and note the time of thisarrival. Then processing means 8 takes the difference between the twotimes (which is directly proportional to the range) and by a knownmathematical algorithm determines the range. In one example, thedifference is multiplied by the speed of sound and this value is used asthe range.

Referring now to FIGS. 6 and 7 there is shown one exemplary type ofembodiment of a hostile weapon location/detection system 2 made inaccordance with the teachings of the invention arid, illustrated anddescribed as used or employed in combination with countermeasure devicesand/or apparatuses. Specifically, FIG. 6 illustrates the exterior of amilitary vehicle 38 with installed components of weapon localizationsystem 2, including microphone array 30, infrared camera 34,repositioning means 22 and a counter-measure device 42. FIG. 7illustrates the components residing in the interior of military vehicle38, including processing means 8, acoustical processor 28, opticprocessor 36, display 44, output line 46 (leading to repositioning means22), output line 48 (leading to counter-measure device 42), input line50 (from microphone array 30), and input line 52 (from infrared camera34).

Weapon location/detection system 2 may also function and/or operate witha camera array 54 (pictured alone in FIG. 8) replacing singular and/orsubstantially singular infrared camera 34. Camera array 54 is designedto have a cumulative field of view of about 360 degrees. In such case,repositioning means. 22 is not included in weapon localization system 2,nor is it required, since camera array 54 covers all possible fields ofview. Other than the absence of repositioning means 22, weaponlocalization system 2 with camera array 54 operates in substantially thesame manner as previously described.

Referring now to FIG. 9, there is shown a weapon location/detectionsystem 56 which represents a second embodiment of the present invention.As shown, weapon localization system 56 includes an acoustical detectionsystem 64, comprising an acoustical processor 68 (which may correspondor be substantially identical to the type of microprocessor assembly asassembly: 28), a microphone array 66; a laser detection system 62,comprising a laser processor and a laser scanner and detector system; aprocessing means 70 (which may correspond to the type of microprocessorassembly as assembly 28); and an output display means 72.

Acoustical detection system 64 may be a conventional and commerciallyavailable acoustical detection system substantially similar topreviously described acoustical detection system 24. Acousticaldetection system 64 operates in substantially the same manner asacoustical detection system 24 with the exception that instead of asingle output transmission, acoustical processor 56 determines thelocation of the source of the acoustical energy and transmits a firstset of data describing such location to processing means 70 and laserprocessor 60, as shown in FIG. 9. Weapon localization system 56 is notlimited to use with acoustical detection system 64. The inventorrealizes, as should one of ordinary skill in the art, that a number ofother acoustical detection systems can be used that would producesubstantially similar results and would not depart from the spirit andscope of the invention as, for example, delineated within the subjoinedclaims.

Laser detection system 62 may be a conventional and commerciallyavailable laser detection system, examples of which are more fullydescribed in the article entitled “Laser Remote Sensing, Air Pollution,”authored by Hun and published by the U.S. Department of Energy (herebyincorporated by reference as if fully and completely set forth herein,word for word and paragraph by paragraph) and sold by OCA Applied Optics(Garden Grove, Calif.) and Laser Technology, Inc. (Englewood, Colo.).

Specifically, laser detection system 62 comprises laser scanner anddetector system 58 and laser processor 60. Laser processor 60 receivesthe first set of data from acoustical processor 68, determines theapproximate direction to the missile trajectory and source and transmitsthis information to laser scanner and detector system 58. Referring nowto FIG. 10, there is shown a block diagram representing laser detectionsystem 62. Laser scanner 74 emits a laser beam which scans the areareceived from laser processor 60. Detector 76 detects the reflectionsoccurring when the laser beam contacts particles, such as aerosols,which are emitted through discharge of a weapon and which are left inthe trail of a missile's trajectory near the muzzle of the weapon.Detector 76 transmits a signal to laser processor 60 which determinesthe location of the source of the hostile weapon fire by eithercalculating the range and azimuth from particles at the point ofdischarge or extrapolating the detected trajectory to an estimatedorigin. Laser processor 60 then transmits a second set of datadescribing such location to processing means 70. Processing means 70will determine values such as azimuth, range, and the trajectory path ofthe incoming missile. The precise operation and calculations ofprocessing means 70, is more fully described in the aforementionedreferences. Weapon localization system 56 is not limited to use with theaforementioned laser detection system. Furthermore, inventor realizes,as should one of ordinary skill in the art, that a number of other laserdetection systems can be used that would produce substantially similarresults and not depart from the spirit of the invention.

To understand the operation of weapon localization system 56, referenceis now made to FIG. 11 which illustrates the operation of the processingmeans 70 used in the preferred embodiment of the invention. In thepreferred embodiment of the invention, processing means 70 is a digitalor analog or combined digital and analog signal processor or amicroprocessor acting under stored program control. Processing means 70will receive first and second sets of data from acoustical detectionsystem 64 and laser detection system 62. Processing means 70 will thenrecord the locations and time of occurrence of each set of data receivedand output the data to a display, as indicated by blocks 78, 80.Processing means 70 will then hold all locations from the first set ofdata for a predetermined period of time and compare with locations fromthe second set of data, as indicated by block 82. A match will beindicated when location and time from the first set of data (hereinafterreferred to as the “acoustical event”) and the second set of data(hereinafter referred to as the “laser event”) fall within apredetermined ranges of each other. If a match is not detected within apredetermined period of time, the unmatching data will be discarded. Ifa match is detected, processing means 70 will generate a signal output,as indicated by block 82. In the preferred embodiment of the invention,the signal output will be transmitted to a display, indicated by block80, where it will be shown in a manner different from the displayedlocations of unmatched data points. In the preferred embodiment of theinvention, a counter-measure device, indicated by block 84, receives thesignal output and is designed to position a weapon and fire acounter-attack at the predicted location of the missile's origin.

Referring now to FIG. 13, there is shown a block diagram of anotherembodiment or “system” of the present invention. Particularly, as shownin FIG. 13, a, top attack detection, tracking and countermeasure system200 may be developed according to the principles of Applicant'sinvention which is especially suited to detect, locate and directcountermeasures against overhead or “top attack” weapons which have beenpreviously described herein and illustrated in FIG. 12. The system 200consists of a detection subsystem 202, which detects the expulsion ofthe two submunitions 106, 108, an active tracking subsystem 204, whichtracks the trajectory of the submunitions 106, 108 as they fall, and acountermeasure subsystem 216 which, in one embodiment, is adapted todirect and control the operation of certain countermeasure deviceseffective to destroy the “incoming submunitions” and to protect thetargeted vehicle and personnel. The system 200 operates by firstdetecting and locating the highest altitude event, (i.e., the “mainevent”, or the event occurring at the highest point of the weapon'strajectory or path) by use of the acoustical detection and locationsystem 218 and the optical, detection and location system 220, whichcollectively sense the acoustical and/or infrared signals associatedwith the main event and/or band-cutting events. The processing functionsand algorithms contained in the above-cited patent references andpublications and as previously explained are used by the system 200 todetermine the direction of the main event and altitude and range of themain event in respect to the vehicle. That information is then used to“cue” and/or control a tracking subsystem 204 that follows the weaponthrough its attack trajectory and facilitates launching a countermeasurevia countermeasure subsystem 216.

The detection and localization subsystem 202 is comprised of a passiveimaging infrared detection device (i.e., optical subsystem 220), apassive acoustical detection device (i.e., acoustical subsystem 218)along with a sensor fusion processor 230. While a combination ofacoustical and optical systems is preferable, it should be understoodthat either one of these technologies (i.e., acoustical or optical)could be used individually as the single detection technology in thisinvention, but with somewhat reduced capability and/or precision. In thepreferred embodiment of system 200, detection subsystem 202 comprisesthe combination and fusion of a passive acoustical detection andlocation system 218 and an infrared.(e.g., mid-wave (3-5 micron))detection and location system 220. Acoustical detection and locationsystem 218 comprises a microphone array 222 and an acoustical signalprocessor 224. Infrared detection and location system 220 comprises oneor more infrared cameras 226, which in this embodiment of the presentinvention are positioned at an “elevated” angle (e.g., approximately 45to 90 degrees) from the horizontal in order to detect the main and/orband cutting events, and an optical signal processor 228. In oneembodiment of the invention, each of the cameras 226 comprisessubstantially identical commercially available cameras such as aninfrared microbolometer sold by the Loral Corporation (Boston, Mass.),or the model IRC-160ST Staring Mid Wavelength Infrared Camera,manufactured and 'sold by Cincinnati Electronics (Cincinnati, Ohio).Sensor fusion processor 230 is substantially similar in function andstructure as previously described processing means 70. As previouslydescribed herein, the dual technology approach exploits the fact thatthe advantages of one technology are the disadvantages of the other sothat by using sensor fusion processing a greatly improved capability andprecision is obtained.

An important feature of the detection and location subsystem 202 of thisinvention is that elevation angle and pattern recognition is applied toboth the optical signals and the acoustic signals received by acousticaldetection and location system 218 and optical detection and locationsystem 220. In such a manner, detection and location subsystem 202provides a means for recognizing and distinguishing the main event andfirst and second “band cutting” events of the overhead weapon 100, fromother ground based weapon attacks and noise. More particularly, insystem 200 both the acoustical detection and location system 218 and theoptical detection and location system 220 are able to discriminateagainst transient acoustic and infrared events associated with groundbased weapons on the basis of elevation angle. A hostile “top attack”weapon would have an elevation angle in the order of 60 degrees or morewhile most other battlefield events and noise would have much lowerelevation angles. Thus, when the acoustical detection and locationsystem 218 detects an elevation angle in the order of 60 degrees orgreater, sensor fusion processor 230 will activate the trackingsubsystem 210. Likewise, when the optical system 220 detects an opticalsignal at an elevation angle in the order of 60 degrees or greater,sensor fusion processor 230 will trigger the tracking subsystem 204.Sensor fusion processor 230 may also be programmed to trigger trackingsubsystem 204 only upon the detection of a 60 degree or greaterelevation angle from both the acoustical detection system 218 and theoptical detection system 220. Triggering of the tracking subsystem 204could also be made further conditional upon receipt of a signal whichmeets predetermined pattern recognition requirements associated with a“main event” and/or “band cutting” events.

Pursuant to the equations and methods described in the above-referencedpatent references and publications, the acoustical detection andlocation system 218 uses the data received by the microphone array 222to calculate the azimuth, angle of elevation, and range of theacoustical signal. The range to the source can also be determinedpassively using the previously described technique of “flash-bang”processing, where the time delay between detection of the flash anddetection of the sound is used to effect the range calculation.

The microphone array 222 is designed to be acoustically semitransparentto allow omnidirectional response for the acoustical hemisphere abovethe ground. Therefore, for a given signal-to-noise ratio there is anapproximately equal probability of detection of transient signalsarriving from any direction. For this application, pattern recognitionwill be optimized for the main event and/or-band cutting events, butwill retain a capability to detect small arms and vehicle mountedweapons as well. This technique has been shown experimentally to becapable of localizing signals generated by all of these sources.

The assumed worst case scenario for the application of acousticaldetection subsystem 218 overhead weapon detection system, is detectionfrom a moving vehicle such as a tank, a cargo truck or a universalutility vehicle (e.g., the “HUM-V”). The dominant noise for a typicalvehicle mounted system is the engine noise assuming proper attention toaerodynamic design to minimize flow noise effects. Results of signaturemeasurements for such vehicles show that a significant amount of theengine and machinery noise can be attenuated by a high pass filter thatgreatly decreases the amplitude of the noise without compromising thesignal amplitude. It should be understood that the acoustical subsystem218 includes a high pass filter.

Fundamental detection theory has shown that the optimum signal detectionis accomplished using a matched filter. A conventional matched filterdesign distinguishes between the background noise and the specificsignal characteristics. In the present invention, the matched filter forthis system will be optimized for the main event and/or the band cuttingevents. It should be understood that acoustical subsystem 218 furtherincludes a matched filter.

In the preferred embodiment of the invention, the optical subsystem 220is sensitive to flashes in the midwave infrared band (3-5 nanometerwavelength). Optical subsystem 220 includes an imaging device ordevices, (i.e., camera 226) that produces a video signal that isanalyzed by optical signal processor 228 to determine the position ofthe detected signal within the field of view. This field of viewinformation is used with camera position and elevation angle informationto relate the position of a detected flash to a three dimensional frameof reference.

In combination, the acoustical system 218 provides weapon positioninformation that allows the sensor fusion processor 230 to distinguishthe flash of the main event and/or the band cutting events from otherfalse flashes. Using the previously described sensor fusion processing,the optical/infrared system 220 provides high accuracy for localizationwhile the acoustical system 218 allows for omnidirectional coverage withsomewhat less accuracy and eliminates false alarms common to theinfrared system. For ambient light conditions where optical contrast islow and optical detection capability is limited, or for conditions ofreduced visibility such as low cloud cover, the presence of tacticalsmoke, and/or tactical overhead cover, the acoustical system 218 alonecan provide sufficient accuracy for effectively detecting, locating andcountering overhead weapon attacks.

The detection and location subsystem 202 is used to cue a trackingsubsystem 204. Tracking subsystem 204 utilizes one or more trackingtechnologies such as (a) a passive visual subsystem (video camera) 246using image tracking processing (one example of such a camera is modelnumber CCD-TRV715 manufactured by Sony), (; (b) a millimeter (mm) waveradar subsystem 242 with and electronically and/or mechanically steeredantenna (one example of such a millimeter wave radar system is describedin Suomela, J., Kuusela, J., and Halme, A. “Millimeter wave radar forclose terrain mapping of an intelligent autonomous vehicle,” 2^(nd) IFACConference on Intelligent Autonomous Vehicles Helsinki, Finland (1995),pp. 349-354, which is fully and completed incorporated herein byreference); (c) a laser radar (e.g., “LADAR”, “LIDAR”, “CLR”, “NLR”)subsystem 244, (examples of such systems are the laser radar systemswhich have been developed and/or are currently in development by theUnited States Air Force Wright Laboratory, Loral Vought Systems, and theLADAR Development and Evaluation Research Facility, and those systemsdescribed in J. W. Grantham, E. C. Meidunas, “Laser Radar in adverseweather,” SPIE Aerosense Conference 3380, Laser Radar Technology andApplications III (1998); E. A. Wachter, W. G. Fisher, “Coherent burstlaser ranging,” SPIE Aerosense Conference 3380, Laser Radar Technologyand Applications III (1998); J. T. Sackos, R. O. Nellums, S. Lebien, J.W. Grantham, T. C. Monson, “Low-cost high resolution video-rate imagingoptical radar,” SPIE Aerosense Conference 3380, Laser Radar Technologyand Applications III (1998); H. N. Burns, S. T. Yun, K. M. Dinndorf, D.R. Hayden, “Compact multichannel receiver using InGaAs APDs forsingle-pulse eye-safe laser radar imagery,” Laser Radar Technology andApplications III (1998); W. J. Mandeville, K. M. Dinndorf, N. E.Champigny, “Characterization of passively Q-switched microchip lasersfor laser radar,” SPIE Vol. 2748, p. 358-366, Laser Radar Technology andApplications, Gary W. Kamerman, Ed. (June 1996); and J. R. Brandt, T. D.Steiner, W. J. Mandeville, K. M. Dinndorf, N. J. Krasutsky, J. L. Minor,“Long-range imaging ladar flight test,” SPIE Vol. 2742, p. 114-117,Applied Laser Radar Technology II, Gary W. Kamerman, Ed. (June 1995) allof which are fully and completely incorporated herein by reference));and/or (d) a mid-wave imaging infrared subsystem 240 with image trackingprocessing, (examples of such systems include the infraredmicrobolometer sold by the Loral Corporation (Boston, Mass.); modelIRC160ST Staring Mid Wavelength Infrared Camera, manufactured and soldby Cincinnati Electronics (Cincinnati, Ohio); or any of the models inthe AGEMA 500 series sold by FLIR Systems, Inc.). It should beunderstood that in a more cost effective embodiment, infrared camera 226and optical signal processor 228 could perform tracking functions aswell as detection functions, thereby replacing and eliminating the need,for infrared subsystem 240. In such case, sensor fusion processor 230would send cueing information back to optical signal processor 228 andinfrared camera 226, and optical signal processor 228 would thencommunicate tracking information directly to tracking fusion processor250. All of the above-listed tracking technologies are commerciallyavailable and well-known in the art.

The detection subsystem 202 provides acquisition information to thetracking system 204. The individual results of tracking subsystems 240,242, 244 and 246 are processed by a tracking fusion processor 250, whichin one embodiment of the invention may be substantially similar toprocessor 70, which calculates the “cueing” information for thecountermeasure. Data such as the time elapsed since the main eventand/or band cutting events, azimuth, elevation/depression angle, arrivalangle and trajectory of the incoming energy can be used to calculate thepath of the submunitions 106, 108. In this manner, tracking fusionprocessor 250 can predict where the location of submunitions 106, 108will be located at some predetermined future time, and cuecountermeasure device 260 to intercept, disable and/or destroy thesubmunitions 106, 108 before they have an opportunity to fire upon thevehicle. Importantly, using the above-listed data, tracking fusionprocessor 260 will be able to determine the most effectivecountermeasure(s) to employ given the time available and the relativeposition of submunitions 106, 108.

Countermeasure device 260 can employ a variety of conventionally knowncountermeasures such as conventional “heat seeking” missiles (e.g.,“patriot” missiles) designed to intercept submunitions 106, 108 anddestroy them before they are able to fire an attack upon the targetedvehicle. Countermeasure device 260 could also deploy tactical smoke orother conventional concealing means to hide the target vehicle from thescanning submunitions 106, 108. One countermeasure device especiallysuited for this application is a directed energy laser which is cued bythe tracking subsystem 204. One example of a suitable directed energylaser system is the Tactical High Energy Laser (THEL) Defense Systemdeveloped by TRW Inc. This directed energy laser is cued in thedirection of a RAID or VRP and is used to cut the fabric of eitherdevice. In this manner, the submunition's timing and arming sequencesare disrupted. When the RAID or VRP is severed, the speed and trajectoryof the subminitions will change, causing the weapons to fall harmlesslyto the ground before their arming sequence can be completed. A directedenergy laser could also be used to directly destroy, submunitions 106,108.

While in the preferred embodiment of the invention, all four trackingsubsystems are utilized, the complete detection, tracking andcountermeasure activation sequence can use different combinations ofthese technologies. For example and without limitation, decreased costconfigurations with substantially similar capabilities are availableusing only selected tracking technologies. An example is shown by theblock diagram in FIG. 14. Here the detection subsystem 302 comprises aninfrared subsystem 320, which is substantially similar to infraredsubsystem 220, and an acoustical subsystem 318, which is substantiallysimilar to acoustic subsystem 218. Detection subsystem 302 is incommunication with a sensor fusion processor 330, which is substantiallysimilar to sensor fusion processor 230 and delivers an output signal tothe tracking subsystem. Tracking is accomplished by the fusion of amillimeter wave radar subsystem 342 and a laser radar tracking subsystem344 via tracking fusion processor 350, which is substantially similar totracking fusion processor 250. Tracking fusion processor 350 “cues”countermeasure device 360 which is substantially similar in function andstructure as countermeasure device 260. Similarly, in anotherembodiment, illustrated in FIG. 15, having only slightly lessperformance but greater ease of implementation, tracking can beperformed by using only millimeter wave radar subsystem 342. Such anapproach would eliminate the need for both laser radar trackingsubsystem 344 and tracking fusion processor 350. Similarly, in theembodiment illustrated in FIG. 15, millimeter wave radar subsystem 342could be replaced with laser radar tracking subsystem 344.

In summary, a wide variety of configurations are possible within thespirit and the scope of this invention. Either detection technologyalone could be used with any combination of one, two, three or all fourtracking technology subsystems. In such an instance, the detectiontechnology would provide acquisition information to the trackingtechnology or technologies. When two or more tracking technologysubsystems ate used, their results would be processed by a trackingfusion processor. This processor would not be necessary for anyconfiguration using a single tracking subsystem. Also included in thespirit of this invention is the use of two or more devices to form asingle technology subsystem. An example would be using two or moreinfrared sensors that are sensitive to two different wavelength signals.Another example would be using two or more lasers with differentwavelengths for threat weapon tracking.

Recent research has shown that the firing of various weapons rangingfrom pistols to cannons causes a burst of radio frequency energy. Also,it is likely that the initial expulsion of a SADARM top-attack weaponemits a similar signal since similar explosive events exhibit suchenergy. It is the purpose of this disclosure to add the capability todetect such radio frequency energy to the previously disclosedAcousto-optic detection system.

For artillery and small arms detection, the added capability willprovide an additional means to confirm the coincidence of weapon firingwith optical events and a means to confirm top attack expulsion events.Further, it will provide a means to determine the specific weapon bymeasuring the frequency of the pulse since frequency is specific to theclass of weapon. This added capability will enhance the capability ofall of the embodiments of the acousto-optic detection system inventionas previously patented.

As shown in FIG. 16, this invention includes an antenna 402 capable ofreceiving radio frequency energy and adds a specific radio frequencyreceiver input 400 to the sensor fusion processor 330 of the combinedoptical and acoustical detection and location technologies 320, 318 thatlocalize the source of hostile weapon fire as previously described. Aswith the previous configuration, the advantages of one technology arethe disadvantages of the other so that by using sensor fusion processinga greatly improved capability is obtained. The technique is applicableto localizing the source of any direct fire weapon that has two or moreof the following signature: optical, acoustic, and/or radio frequencyburst. Non-limiting examples of such weapons include small arms, shortrange missiles, rockets, small caliber mortars, and large artillery. Anadded advantage is “flash-bang” processing in that the differencebetween the time of occurrence of the flash and the time of arrival ofthe acoustic signal can be measured to determine the range to thehostile fire location by exclusively passive means.

Various embodiments of uncooled microbolometer imaging infrared camerasare also claimed for this invention. A microbolometer comprises an arrayof a resistive material that has a specific electrical resistance of aspecific value for the dark condition or not receiving infraredradiation. When receiving infrared radiation, commonly in the 3-5 micronband or in the 8-14 micron band, the resistance of the individualelements in the array changes in a manner corresponding to the amount ofradiation received. Such a camera would be a significant enhancement tothe invention as previously described and as modified here. Specificdesigns include the LTC 500 and its imaging module and the SIM200 ascurrently marketed by BAE Systems, previously Lockheed Martin andSanders Associates, a Lockheed Martin Corporation.

A second infrared camera claimed with this invention is an uncooledinfrared detector based upon bandgap detection and described in U.S.Pat. 6,114,696 and a third is the uncooled infrared bandgap detectordescribed in U.S. Pat. 6,100,525, both assigned to the Lockheed MartinCorporation. Such a camera would be a significant enhancement to all ofthe basic embodiments of the acousto-optic detection system inventionthat include an infrared camera.

The two bandgap detector devices are described as follows. An infraredradiation detection device that comprises a dipole antenna mounted on asubstrate and connected through blocking contacts to a bandgap detectorelement. The dipole antenna has a length which is approximately one halfthe wavelength of the incident infrared radiation. The bandgap detectorelement has linear dimensions which are each substantially smaller thanthe wavelength of the detected radiation. A group of detector devicesare combined to form an array which can produce a device that is capableof producing a usable output signal without the need for cooling belowambient temperature. Such an array forms the sensing element fromimaging an infrared source such as the flash of a rifle, machine gun,SADARM expulsion or and artillery weapon.

Another possible embodiment is to use a single directional microphone ofvarious constructions to be used to find the approximate direction tothe source of hostile weapon fire. While not as accurate as thepreviously described, multiple microphone array formed fromomnidirectional microphones, this means can be used to confirm directionas determined by an optical or electro-optical (laser) detection sensoras was described previously.

It is to be understood that the invention is not limited to the exactconstruction or method illustrated and described above, but that variouschanges and modifications may be made without departing from the spiritand scope of the invention as defined in the following claims. Moreover,it should be realized that Applicant's weapon location system inventionis superior to those of the prior art in that Applicant has combined twodissimilar types of weapons location systems in order to produce asystem providing highly superior results which has hereto before notbeen obtainable.

What is claimed is:
 1. A weapon localization system adapted to determinethe location of weapon fire, said system comprising: acousticaldetection and direction sensing means for detecting energy of a firstfrequency originating from said weapon fire, and for transmitting afirst set of data describing direction to said weapon fire and time ofdetection of said energy of a first frequency; and optical detection anddirection sensing means for detecting and sensing direction to energy ofa second frequency originating from said weapon fire, and fortransmitting a second set of data describing said direction to saidweapon fire and time of detection of said energy of a second frequency;and radio frequency detection means for detecting energy of a thirdfrequency originating from said weapon fire, and for transmitting athird set of data describing said time of detection of said energy of athird frequency; and a first processing means coupled to said acousticaldetection and direction sensing means, and said optical detection anddirection sensing means, for receiving said first set of data, and saidsecond set of data, and for determining whether said direction describedby said first set of data match said direction described by said secondset of data and for generating a signal output if said match occurs; anda second processing means coupled to said optical detection anddirection sensing means, and said radio frequency detection means, forreceiving said second set of data and said third set of data, and fordetermining whether said time of detection described by said second setof data match said time of detection described by said third set of dataand for generating a signal output if said match occurs.
 2. The weaponlocalization system of claim 1 wherein said acoustical detection anddirection sensing means comprises an array of one or more directionalmicrophones.
 3. The weapon localization system of claim 1 wherein saidacoustical detection and direction sensing means comprises an array ofone or more non-directional microphones.
 4. The weapon localizationsystem of claim 1 wherein said optical detection and direction sensingmeans comprises an infrared imaging camera.
 5. The weapon localizationsystem of claim 4 wherein said infrared imaging camera comprises anuncooled microbolometer.
 6. The weapon localization system of claim 4wherein said infrared imaging camera comprises an uncooled infraredimaging bandgap detector camera.
 7. The weapon localization system ofclaim 4 wherein said infrared imaging camera comprises a quantum wellinfrared imaging camera.
 8. The weapon localization system of claim 1wherein said radio frequency detection means comprises a radio receiver.9. The weapon localization system of claim 1 wherein said radiofrequency detection means comprises a spectrum analyzer.
 10. A methodfor determining the distance from the weapon localization system ofclaim 1 to location of said weapon fire were the initial direction tosaid weapon is unknown, said method comprising the steps of: (a) Sensingoptical energy generated from said weapon fire; (b) Sensing acousticalenergy generated from said weapon fire; (c) Determining a first time atwhich said optical energy was sensed; (d) Determining a second time atwhich said acoustical energy was sensed; (e) Determining a differencebetween said first and said second times; and (f) Calculating said rangeby use of difference between said first and said second times.
 11. Amethod for determining the distance from the weapon localization systemof claim 1 to location of said weapon fire were the initial direction tosaid weapon is unknown, said method comprising the steps of: (a) Sensingradio frequency energy generated from said weapon fire; (b) Sensingacoustical energy generated from said weapon fire; (c) Determining afirst time at which said radio frequency energy was sensed; (d)Determining a second time at which said acoustical energy was sensed;(e) Determining a difference between said first and said second times;and (f) Calculating said range by use of difference between said firstand said second times.
 12. The weapon localization system of claim 1wherein said optical detection and direction sensing means comprisesoptical imaging transducer means and optical reflection means that arefixed in relative physical positions such that said energy of a secondfrequency originating from said weapon fire and incident on said opticalreflection means from any horizontal direction and any elevation anglebetween 90 degrees above a horizontal plane and 10 degrees below saidhorizontal plane is sensed by said optical imaging transducer means andforms an image on said optical imaging transducer means at a locationthat uniquely corresponds to the direction to said weapon fire; and athird processing means coupled to said optical imaging transducer meansadapted to receive a fourth set of data from said optical imagingtransducer means and determine direction to said weapon fire and fortransmitting a fifth set of data describing said time of detection ofsaid energy of a second frequency and said direction to said weaponfire.
 13. The weapon localization system of claim 12 wherein saidoptical reflection means comprises a reflector with the shape of a cone.14. The weapon localization system of claim 12 wherein said opticalreflection means comprises a reflector with the shape of a hyperboloid.15. The weapon localization system of claim 1 wherein said opticaldetection and direction sensing means comprises optical imagingtransducer means and an optical refraction means that are fixed inrelative physical positions such that said energy of a second frequencyoriginating from said weapon fire and incident on said opticalrefraction means from any horizontal direction and any elevation anglebetween 90 degrees above a horizontal plane and 10 degrees below saidhorizontal plane is sensed by said optical imaging transducer means andforms an image on said optical imaging transducer means at a locationthat uniquely corresponds to the direction to said weapon fire; and afourth processing means coupled to said optical imaging transducer meansadapted to receive a sixth set of data from said optical imagingtransducer means and determine direction to said weapon fire and fortransmitting a seventh set of data describing said direction to saidweapon fire and time of detection of said energy of a second frequency.16. The weapon localization system of claim 1 wherein said opticalrefraction means comprises a wide angle lens.
 17. The weaponlocalization system of claim 12 wherein said optical refraction meanscomprises a reflector with the shape of a parabaloid.
 18. The weaponlocalization system of claim 12 wherein said optical optical imagingtransducer means comprises an ultraviolet imaging camera.
 19. The weaponlocalization system of claim 12 wherein said optical imaging transducermeans comprises an infrared imaging camera.
 20. The weapon localizationsystem of claim 12 wherein said optical imaging transducer meanscomprises a visual imaging camera.
 21. The weapon localization system ofclaim 1 wherein said weapon localization system comprises a top attacklocalization system.
 22. The weapon localization system of claim 1wherein said weapon localization system comprises a sniper localizationsystem.
 23. A weapon localization system as in claim 1 comprising anacoustic receiver; an optical receiver; a radio frequency receiver; aprocessor coupled to each of said receivers; and an information display.24. A weapon localization system as in claim 1 comprising one or moreacoustic receivers; one or more optical receivers; one or more radiofrequency receivers; a processor coupled to each of said receivers; andan information display.
 25. A weapon localization system as in claim 1comprising an acoustic receiver; one or more optical receivers; aprocessor coupled to each of said receivers; and an information display.26. A weapon localization system as in claim 1 comprising one or moreacoustic receivers; one or more radio frequency receivers; a processorcoupled to each of said receivers; and an information display.
 27. Aweapon localization system as in claim 1 comprising one or more opticalreceivers; one or more radio frequency receivers; a processor coupled toeach of said receivers; and an information display.
 28. A weaponlocalization system as in claim 1 comprising one or more opticalreceivers; one or more radio frequency receivers; a processor coupled toeach of said receivers; and an information display.